Author Topic: Airspeed in IAS or TAS?  (Read 189 times)

Offline blur

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Airspeed in IAS or TAS?
« on: October 11, 1999, 07:20:00 AM »
Maybe this has already been discussed but I can't find any previous posts that cover this issue.

I took a clean Spit IX up to 25k and with WEP obtained 410 mph on the airspeed indicator. If this is IAS my TAS would be 589.4 mph! It seems that the airspeed is in TAS because most sources give the mark IX a TAS of 408 mph at this altitude. Unless my math is wrong an IAS of 284 mph will give a TAS of 408 mph.

Any aeronautical engineers out there?

Offline hitech

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Airspeed in IAS or TAS?
« Reply #1 on: October 11, 1999, 07:31:00 AM »
All planes are supposed to be showing IAS. The spit has a bug that its displaying TAS at the moment.

HiTech

Offline blur

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Airspeed in IAS or TAS?
« Reply #2 on: October 11, 1999, 07:54:00 AM »
Aw shucks, I was getting ready to BnZ ME262's!  

Thanks for quick reply.

Offline RASTER

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Airspeed in IAS or TAS?
« Reply #3 on: October 12, 1999, 05:59:00 PM »
Suspect some head winds could account for a True Air Speed (TAS)[relative to ground travel] and Indicated Air Speed (IAS)[relative to surrounding air]difference of 100mph. Think turning sideways would be almost fatal though. Was Floyd being programed into Aces High?

RASTER

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Airspeed in IAS or TAS?
« Reply #4 on: October 13, 1999, 12:21:00 AM »
  Ummm, Rast...I think we're a bit confused about the differences in speeds...

IAS (Indicated airspeed)-what the guage reads

CAS (Calibrated Airspeed)-IAS corrected for installation errors and such (like when flap settings have an effect on the reading and stuff)

TAS (Ture Airspeed)-how fast you're actually going through the air.  Basically, since the air is not always the same density (due to local atmospheric pressure, temperature...), the airspeed indicator doesn't always indicate correctly.  At 25,000 feet on a hot day, there's a lot less air density with which to push on the bellows, thus creating a reading as it would at a lower speed at lower altitude...  Think about it, it'll make sense (the same reason the A/C loses performance at altitude makes the IAS read low).

Groundspeed-how fast the aircraft moves across the ground.  You use TAS and your course to figure this out by figuring int he winds aloft (direction and speed).  You can figure that out geometrically, but I've got a handy flight computer (3 of em actually)...moot point in AH anyway, seeing no winds aloft...

blk  (AT)

PS-IAS is what we fly by (duh).  Basically, because the airplane will always stall at the same IAS in the same conditions (1 G, wings level...)  since the thin air that would make it stall at a higher TAS is also affecting the airspeed indicator...  Think about it...it'll make sense (I didn't totally get it until I was just about to solo)